AU613185B2 - Extrudable multi-durometer hydrodynamic bearing and method of making the same - Google Patents

Extrudable multi-durometer hydrodynamic bearing and method of making the same Download PDF

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AU613185B2
AU613185B2 AU33892/89A AU3389289A AU613185B2 AU 613185 B2 AU613185 B2 AU 613185B2 AU 33892/89 A AU33892/89 A AU 33892/89A AU 3389289 A AU3389289 A AU 3389289A AU 613185 B2 AU613185 B2 AU 613185B2
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bearing
skeletal
pad
bearings
segments
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AU3389289A (en
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Russell D. Ide
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    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16CSHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
    • F16C33/00Parts of bearings; Special methods for making bearings or parts thereof
    • F16C33/02Parts of sliding-contact bearings
    • F16C33/04Brasses; Bushes; Linings
    • F16C33/06Sliding surface mainly made of metal
    • F16C33/14Special methods of manufacture; Running-in
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16CSHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
    • F16C33/00Parts of bearings; Special methods for making bearings or parts thereof
    • F16C33/02Parts of sliding-contact bearings
    • F16C33/04Brasses; Bushes; Linings
    • F16C33/22Sliding surface consisting mainly of rubber or synthetic rubber
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B63SHIPS OR OTHER WATERBORNE VESSELS; RELATED EQUIPMENT
    • B63HMARINE PROPULSION OR STEERING
    • B63H23/00Transmitting power from propulsion power plant to propulsive elements
    • B63H23/32Other parts
    • B63H23/321Bearings or seals specially adapted for propeller shafts
    • B63H23/326Water lubricated bearings
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16CSHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
    • F16C17/00Sliding-contact bearings for exclusively rotary movement
    • F16C17/02Sliding-contact bearings for exclusively rotary movement for radial load only
    • F16C17/03Sliding-contact bearings for exclusively rotary movement for radial load only with tiltably-supported segments, e.g. Michell bearings
    • F16C17/035Sliding-contact bearings for exclusively rotary movement for radial load only with tiltably-supported segments, e.g. Michell bearings the segments being integrally formed with, or rigidly fixed to, a support-element
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16CSHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
    • F16C32/00Bearings not otherwise provided for
    • F16C32/06Bearings not otherwise provided for with moving member supported by a fluid cushion formed, at least to a large extent, otherwise than by movement of the shaft, e.g. hydrostatic air-cushion bearings
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16CSHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
    • F16C2326/00Articles relating to transporting
    • F16C2326/30Ships, e.g. propelling shafts and bearings therefor

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  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Ocean & Marine Engineering (AREA)
  • Sliding-Contact Bearings (AREA)
  • Support Of The Bearing (AREA)
  • Magnetic Bearings And Hydrostatic Bearings (AREA)
  • Organic Low-Molecular-Weight Compounds And Preparation Thereof (AREA)
  • Complex Calculations (AREA)
  • Heterocyclic Carbon Compounds Containing A Hetero Ring Having Nitrogen And Oxygen As The Only Ring Hetero Atoms (AREA)
  • Lubricants (AREA)
  • Detergent Compositions (AREA)
  • Extrusion Moulding Of Plastics Or The Like (AREA)
  • Compounds Of Unknown Constitution (AREA)
  • Manufacture Of Porous Articles, And Recovery And Treatment Of Waste Products (AREA)
  • Powder Metallurgy (AREA)
  • Extrusion Of Metal (AREA)

Abstract

An extrudable multi-durometer hydrodynamic bearing which includes a bearing pad support structure (10) and a plurality of bearing pads (50) fused to the bearing pad support structure (10). The bearing may also include a number of deflection control members (80) fused to the bearing pads and/or the bearing pad support structure. The pad supports of the bearing and movable with six degrees of freedom. The bearing is constructed entirely of non-newtonian fluidic materials and has a constant axial cross-section so that it may be easily extruded. The bearing includes portions having different hardnesses. The method of making the bearing includes the steps of extruding a first material, extruding at least a second material onto the first material prior to curing the first material forming a tubular extrusion, curing the tubular extrusion, cutting the tubular extrusion into bearing segments and sizing the bearing segments by machining the individual bearing segments to the desired inner and outer diameters.

Description

COMMONWEALTH OF AUSTRALIA6 Patent Act 1952 COMPLETE SPECIFICATION
(ORIGINAL)
Class Int. Class Application Number Lodged Complete Specification Lodged Accepted Published 'Priority Related Art 0 6 Name and Address of Applicant Actual Inventor Address for Service Russell D. Ide 28 Daniel Drive, Coventry, Rhode Island, 02816-0744 United States of America.
Russell D. Ide FREEHILL HOLLINGDALE PAGE BHP HOUSE, 140 WILLIAM STREET, MELBOURNE. AUSTRALIA. 3000.
TEL:
FAX:
(Our (03) (03) Ref: 640 2640 640 2689 JIM;:WMcM:1321975) Complete Specification of the invention entitled: EXTRUDABLE MULTI-DUROMETER IIYDRODYNAMIC BEARING AND METHOD OF MAKING TIHE SAME The following is a full description of this invention including performing it known to me:the best method of 1880321/WF188 01/05/89 1 a- EXTRUDABLE MULTI-DUROMETER HYDRODYNAMIC BEARING AN'D METHOD OF MAKING THE SAME Background of the Invention The present invention relates to hydrodynamic bearings. In such bearings, a rotating object such as a shaft is supported by a stationary bearing via a pressurized fluid such as oil, air or water.
00 0 00 0 0Hydrodynamic bearings are often, but not exclusively, o employed in so-called process lubricated applications in 00 which the beaxing is lubricated by the available fluid 0 0 0 000 rather than a~ typical lubricant such as oil. specific 0 00 applications include pump line shaft bearings which may :0000 be lubricated by the fluid being pumped or marine shaft bearings which are lubricated by water.
000 0 0 0 0 Hydrodynamic bearings take advantage of the 0 00 slide along the top of the fluid. Instead, the fluid in 0 00d 000 ~0 contact with the rotating object adheres tightly to the rotating object, and motion is accompanied by slip or shear between the fluid particles through the entire 0 height of the fluid film. Thus, if the rotating object and the conta- ting layer of fluid move at a velocity which is knowr, the velocity at intermediate heights of the fluid thickness decreases at a known rate until the fluid in contact with the stationiary bearing pad adheres to the bearinq pad and is motionlLass. When, by virtue of -2the load resulting from its support of the rotating object, the bearing pad is deflected at a small angle to the rotating member, the fluid -will be drawn into the wedge-shaped opening, and sufficient pressure will be generated in the fluid film to support the load. This fact is utilized in thrust bearings for hydraulic turbines and propeller shafts of ships, as well as in the conventional journal bearing with fluid lubrication.
Although oil is typically the fluid of choice for heavy loads, lighter loads can be supported with other fluids such as air or water.
The bearings of the present invention can be used as a substitute for the so-called cutless style or wear-type rubber bearings commonly employed in marine and other applications. Although, these cutless or wear-type bearings include a water wedge to achieve a 00r hydrodynamic effect, they suffer from a number of structural limitations and inevitably experience wear.
0 00 C0 0 As discussed below, the inventor has discovered that the 0000 limitations of these bearings are primarily attributable 0*0000to their structure which consists of a relatively large 0 0 0000 0 cross section of soft single durometer rubber mounted in a 0 a cylindrical metal tube. Because of the softness of the rubber and the relatively large axial cross section a0: of the soft rubber, this bearing has insufficient radial ,0,00 stiffness to achieve optimum performance.
4 CeThe present invention also relates to a hydrodynamic bearing having beam-mounted bearing pads.
A good example of a beam-mounted bearing pad is disclosed in U.S. Patent 3,107,955 to Trumpler. In such bearings, the hydrodynamic bearing pad is mounted on beam-like supp.)rt members so that the pad can deflect to form a hydrodyniamic wedge.
Although hydrodynamic bearings and beam-
I
-3mounted bearing pads have been known for some time, it is only recently, with the assistance of computer aided finite element analysis, that the present inventor has discovered the tremendous significance of the relatively small deflections which occur when hydrodynamic bearings are loaded. Aside from a limited number of exceptions such as U.S. Patent No. 3,107,955 to Trumpler, these deflections, which are difficult to physically measure, had previously been regarded as insignificant and/or ignored by bearing designers. However, the present inventor has discovered that by modeling the performance of hydrodynamic bearings on computers the deflections can be predetermined and bearings having dramatically improved performance characteristics can be designed.
These bearings can be generally characterized as including at least one beam-mounted bearing pad.
Examples of such improved bearings are described in the 0o6 0 inventor's previous U.S. Patents Nos. 4,496,251; 0° 4,526,482 and 4,676,668.
.000 o o 0 04 0 00000 U.S. Patent No. 4,496,251 discloses, among 0. other things, a bearing which includes a pad which 0 0 0o0 o0 deflects with web-like ligaments so that the wedge 0 shaped film of lubricant is formed between the relatively moving parts.
oo0 0 Q0 60 00 M 6 C U.S. Patent 4,515,486 discloses, among other 00 things, hydrodynamic journal and thrust bearings which 0 comprise a number of bearing pads, each pad having a face member and a support member that are separated and bonded together by an elastomeric material.
C
U.S. Patent No. 4,676,668 discloses, among other things, a bearing in which the bearing pads may be spaced from the support member by at least one leg which provides flexibility in three directions. To provide flexibility in the plane of motion, the legs are angled
%I
-4inward to form a conical shape with a point of intersection in front of the pad surface. Each leg has a section modulus that is relatively small in the direction of desired motion to permit compensation for misalignment Finally, U.S. Patent No. 4,526,482 discloses, among other things, a hydrodynamic bearing which is primarily intended for process lubricated applications, the bearing is designed to work in a fluid. The hydrodynamic bearing is formed with a central section of the load carrying surface that is more compliant than the remainder of the bearing so that it will deflect under load and form a pressure pocket of fluid to carry high loads.
The bearings described in the aforementioned :1 0 patent are typically at least partially metallic and S° have shapes which cannot be easily extruded but have d o been found to .e most suitable for certain applications.
044 oo Nevertheless, these bearings can typically be produced o" o.at cost far below those of bearings with similar 0 V performance capabilities. This is because the bearings of the present invention are typically both less complex than competitive bearings and smaller than competitive bearings. Moreover, these bearings exhibit remarkably improved wear characteristics. This improved performance is primarily attributable to the designers appreciation of the forces the bearings will be subject to and the resulting bearing design which accommodates cthe forces.
Despite the many advantages and economies associated with these bearings, it is desirable to find a way to redace further the cost of producing such bearings. This is particularly true in those contexts in which the high performance of the bearings described in
I
~Y -r the applicant's previous patents is not required.
The present invention also relates to the use of non-newtonian fluids such as plastic, rubber and the like in hydrodynamic bearings. Non-newtonian fluids are characterized as real fluids. All real fluids have internal friction so that their rate of deformation is proportional to the applied shear stress. If the rate of deformation is directly proportional, it is called a newtonian fluid if not, the fluid is called a nonnewtonian fluid. Thus, non-newtonian fluids may be generally characterized as fluids whose viscosity changes with rate of flow. The use of non-newtonian fluidic materials offers unique advantages and presents significant obstacles by virtue of the unique characteristics of the non-newtonian fluids.
For instance, when a non-newtonian fluid such as plastic or rubber is restrained, it becomes So incompressible. However, when the same material is o unrestrained it flows in a predictable manner in response to an applied load. Furthermore, non-newtonian fluidic materials such as rubber, plastic or the like are typically less expensive than the metallic materials generally employed in bearing construction. Manufacture o of non-newtonian fluidic material parts is typically o easier than manufacture of comparable metallic parts.
l ,Despite the many advantages expected to accrue from the use of non-newtonian fluidic materials in hydrodynamic bearings, such materials have only been used to a limited extent.
Summary of the Invention The present invention is a hydrodynamic bearing suitable for use in process lubricated as well t_ IYCIYL- L -A -6as other applications and a method of making the bearing. The bearing has a constant cross-section so that it can be easily extruded, it has an extrudable shape. The bearing includes a plurality of beam-mounted bearing pads. Additionally, the bearing is extruded as a composite of tL-. or more non-newtonian, preferably elastomeric or polymeric, -rterials such as plastic, rubber or the like having varied stirinesses, in other words, a multi-durometer composite plastic so as to achieve the benefits of varied stiffness.
More specifically, the bearing of the present invention is an extrudable multi-durometer hydrodynamic bearing. The bearing is constructed entirely of nonnewtonian fluidic materials and has an extrudable axial cross-section. The bearing includes a generally circumferential skeletal bearing pad support portion o having a predetermined hardness. The skeletal portion U has inner and outer circumferential surfaces. A 0 o 2 plurality of i.iner axial grooves are formed in the inner o surface and a plurality of outer axial grooves are So"°o formed in the outer surface. The inner axial grooves 0 I and the outer axial grooves are spaced with respect to one another to define a plurality of beam-mounted bearing pad support surfaces. Th- bearing also includes a plurality of bearing pads having a predetermined 0 hardness which is less than the predetermined hardness of the skeletal portion. Each of the bearing pads is I fused to a corresponding bearing pad support surface.
The bearing may also include deflection control members fused into the inner grooves and/or the outer grooves.
The deflection control members are preferably softer than the skeletal bearing pad support portion.
The inventor has discovered that in many specific applications such as in high speed applications, it is necessary to examine and evaluate A A ii7-
II
the dynamic flexibility of the entire system consisting of the shaft or rotor, the hydrodynamic lubricating film and the .bearing. In computer analysis of this system using a finite element model, it has been determined that it is necessary to treat the entire bearing as a completely flexible member that changes shape under operating loads. By adding more or less flexibility via machining of the basic structure, bearing characteristics may be achieved that provide stable low friction operation over wide operating ranges. A number of variables have-been found to substantially affect the bearings performance characteristis. Among the most important variables are the shape, size, location and material characteriscs modulus of elasticity etc.) of the pad and support members of the hydrodynamic bearing. The shape of the support members has been found to be particularly important.
0 0° The present invention also relates to a 0000 0 hydrodynamic bearing having a plurality of bearing pads '0 0 0 0 oo' formed of a relatively soft non-newtonian fluidic 00 0, material. The bearing pads have arc shaped or concave 0,o faces and are constrained so as to deflect under the 4 load normally applied by a supported shaft, in a manner which provides a wedge shaped gap between the shaft and the arc shaped face of the bearing pad.
S4P By virtue of the varying stiffnesses, the bearing exhibits improved performance characteristics.
In particular, the use of stiff as well as soft flexible non-newtonian fluidic materials allows the bearing to retain sufficient stiffness to ensure proper formation of a hydrodynamic wedge. Thus, the present invention obviates the problems experienced with known cutless or wear-type bearings.
Moreover, by virtue of its construction of relatively inexpensive non-newtonian fluidic materialr preferably elastomeric or polymeric materials such as plastic, rubber or the like and its ability to be extruded, the bearing can be produced at significantly lower costs than other non-extrudable bearings. In fact, preliminary indications suggest that the bearing can be produced in quantity for less than 1% of the cost of competitive marine style bearings.
The present invention also takes advantage of the physical characteristics associated with nonnewtonian fluids. For example, as noted, above certain non-newtonian fluids such as polymers and elastomers become incompressible when restrained. The present invention provides a hydrodynamic bearing constructed entirely of non-newtonian fluids having a plurality of sections, the sections having significantly different U durometers (hardnes3es or stiffnesses). The sections are formed such that a first, harder, section restrains a 0 0 o o second softer section so that the second section is 0 .00 stiff, substantially incompressible in the radial 0 0 "direction but flexible in the shear direction. By 0 00 oproviding the softer sections and harder sections so as ato define a plurality of relatively soft, concave, beam-mounted bearing pads mounted relatively rigid beam-mounted bearing pad support faces the bearing 0 °°becomes shaped so as to deflect in a known manner to provide a hydrodynamic wedge to support a rotating 04 shaft.
The bearing of the present invention is suitable for use in many applicat:ons. However, the bearing is particularly well suited for use in process lubricated applications such as oil well drilling applicatinns, submersible or turbine pump applications and marine drive shaft applications.
4! 03 0 3 03o 3 31?, 33430 3 a 33 0 I o 0 1 0 2 aa 0P 0 6 40 0 04 -9- The bearing is extruded using known multidurometer extrusion techniques which are commonly employed in extruding multi-durometer plastic components such as window and door seals, shock absorbing bumpers, and flexible hinges, but have, to applicant's knowledge, not yet been utilized to manufacture bearings.
When utilized to extrude multi-durometer pieces such as the' bearings of the present invention, the technique would typically involve a method in which the multi-durometer sections are successively extruded onto one another in a partially cured or uncured state such that no adhesive is required to form the composite extrusion. This is because in the partially cured or uncured state, the extruded materials are inherently gummy or tacky. After the complete tubular section is extruded, the entire extrusion is cured to yield a composite tubular member having multiple sections of varying stiffness durometer). In the instance of the bearings of the present invention, the relatively long extrusion having the requisite axial cross-section and appropriate multi-duromneter sections is extruded and then cut to form individual bearings. The individual bearings are sized by machining to, among other things, precisely define the required inner diameter and outer diameter.
Brief Description of the Drawings Figure 1 is an axial cross-section of a bearing in accordance with the present invention.
Figure 2 is a perspective view of a tubular extrusion in accordance with the present invention.
Figure 3 is an enlarged partial axial crosssection of a bearing in accordance with the present -1 invention.
Figure 4 is a partial cross-section illustrating a bearing according to the present invention deflecting under the load of a rotating shaft.
Figure 5 is a diagram of the general steps employed in manufacturing a bearing according to the method of the present invention.
Detailed Description of the Drawings FIG. 1 is a cross-section of a typical extrudable bearing in accordance with the present invention. In the example illustrated, the bearing is considered extrudable because it has a constant axial cross-section as viewed in FIG. 1.
06 0 0 oB 0 0 aAs illustrated in FIG. i, the bearing has been 0*00 0 0 0° 0 machined to the precise required outer diameter O.D. and 0 a o0o .inner diameter I.D. The phantom lines in FIG. 1 9 oo illustrate the inner and outer diameter after extrusion prior to machining. In a normal use, the bearing is e placed in a housing which intimately contacts the outer diameter of the bearing and the bearing supports a shaft "o located within the inner diameter of the bearing.
4 4 Accordingly, the outer diameter of the bearing is a function of the inner diameter of the housing into which the bearing is to be located and the inner diameter is a function of the size of the shaft to be supported. Of course, as with any hydrodynamic bearing, the inner diameter of the bearing is a predetermined amount larger than the outer diameter of the shaft which is to be supported by the bearing so as to allow a fluid film which supports the shaft.
As shown in FIG. 1, the bearing of the present -11invention is constructed entirely of non-newtonian fluidic materials preferably polymeric or elastomeric materials such as a rubber, plastic or the like. The bearing consists of a composite of sections of nonnewtonian fluidic materials having different hardnesses.
Specifically, the bearing includes a unitary beam-like skeletal pad support portion 10 constructed of a relatively rigid or hard material, for example, hard durometer shore D rubber. The skeletal pad support portion 10 is generally circumferential in shape and includes a plurality of circumferentially spaced radially outwardly extending inner axial grooves 12 formed on the bearings inner circumferential surface and circumferentially spaced radially inwardly extending outer axial grooves 14 formed on the bearings outer circumferential surface. By virtue of these grooves, the skeletal pad support portion 10 of the illustrated bearing has a somewhat cogged discontinuous o circumferential appearance.
Q 00 SThe particular shape of the bearing o o 0illustrated in FIG. 1 is by no means essential to the 0 present invention and in fact is desirable for only 0 specific applizations. The specific cross-section of the bearing in accordance with the present invention for any o particular application depends on the deflections o required to achieve optimum results. Thus, in certain instances it may be desirable to provided a bearing t which does not include outer axial grooves such as those shown at 14 in FIG. 1. Moreover, the grooves could have various cross-sections, more or less tapered, to achieve the most desirable functions under load.
When the bearing of the present invention is provided with both inner and outer axial grooves and when the inner grooves are located between adjacent outer grooves as illustrated in FIG. i, the skeletal pad -12support structure functions as a network of essentially circumferentiaL, and radial beams adapted to deflect under load. FIG. 3 illustrates a portion of the beam network for a portion of a bearing similar to that shown in FIG. 1. The bearing shown in FIG. 1 includes eight bearing pad support sectors or segments. The pad support sectors or segments are defined by the spaced inner axial grooves 12. Each pad support sector or segment includes an arcuate bearing pad support face 16 defined by the radially innermost surface of the pad support segment, a housing contacting surface 18 defined by the radially outermost portions 18 of the pad support segments and a pair of connecting portions 20 connecting the housing contacting portions 18 with the bearing support face 16. By virtue of this construction, the skeletal pad support portion 10 functions as a network of beams as illustrated in FIG. 3. The network of beams includes the inner circumferential beams illustrated at o 26, the outer circumferential beams illustrated at 28 o o and the radial beams illustrated at 30. Under load' this 0 0 network of "'eams deflects in a manner which is 0oU0 determinable based upon the degree of the load, the material used in the skeletal pad support structure S and the ,ize ind spacing of the inner and outer axial grooves.
nao a a OOa aAt this point it should be noted that although the non-newtonian fluidic material used in the skeletal SBOr pad support portion 10 is described herein as relatively rigid or hard as compared to the relatively flexible or soft materials used in other portions of the bearing described below, the material used to form the skeletal pad support portion 10 is significantly more flexible than the metals which typically form the skeletal portions of jcurnal or sleeve bearings. Accordingly, it is to be expected that the skeletal portion of the bearings of the present invention deflect under load to -13a far greater degree than bearings having metallic celetal portions. A typical skeletal material in the present invention would have a hardness on the Shore D scale.
Referring to FIG. 1, the bearing of the present invention also includes a plurality of relatively soft or flexible bearing pads corresponding in number to the number of bearing pad support surfaces provided on the skeletal portion In accordance with an important aspect of the present invention, the bearing pads are preferably fused to the skeletal portion. The bearing pads 50 are concave in cross-section as shown in FIG. 1 and are somewhat radially thicker in the middle and arcuately taper inward toward their circumferential ends. The reason for this thicker middle and thinner end portion is to facilitate deflection of the bearing pad under load. The 4 4 bearing pads 50 are formed of a relatively soft or 6 4 4 flexible non-newtonian fluidic material, preferably a oo polymer or elastomer such as rubber, plastic or the 0 like. For example, the bearing pads 50 may be 0 constructed of durometer Shore A rubber. The material o used to form the bearing pad is preferably substantially softer or more flexible than the material used to form af, the skeletal portion 10. The softer material provides better performance and reduces shaft wear in low viscosity or abrasive lubricant operating conditions.
Since both the skeletal portion 10 and the bearing pads 50 are constructed of non-newtonian fluids, they tend to flow in a determinable manner under load.
In a typical usage situation, the bearing is subject to both radial loads resulting from the weight of the shaft and shear loads resulting from the rotation of the shaft. Since the bearing is restrain-d in the radial direction by a housing in normal usage, the fluidic j-U C ~YI ~L-31~11I The fo.lowing is a fLy1 description of this invention including the best method of performing it known to me:- 1880321/WF188 01/05/89 1 -14materials of which the bearing is constructed are incompressible in the radial direction. However, this is true only to the extent the bearing is restrained by the housing in the radial direction. For instance, if the outer axial grooves 14 are not filled, with deflection control members, as described below, portions along the outer circumference cf the bearing are not restrained by the housing in the radial direction. Accordingly, some radial deflection of the bearing can occur.
When the bearing is entirely restrained in the radial direction by the housing, it is nearly inccrpressible in the radial direction and the radial load is absorbed by the fluid film between the bearing pads 50 and the rotating shaft. On the other hand, by virtue of the inner axial grooves 12, neither the bearing pads nor the skeletal portion 10 is restrained from circumferential deflection in response to the shear load applied by the rotating shaft. Moreover, since there is a gac between the shaft and the radially inner most surface of the bearing pads 50, the entire bearing pad 50 and the associated segment of the skeletal portion 10 can swing upward in response to the shear load applied by the rotating shaft to form a hydrodynamic wedge. An example of such deflection (greatly exaggerated is illustrated in FIG. 4. Of course, because the material used in the bearing pad is much softer and more flexible than the material used in the skeletal portion 10, the bearing portions deflect or flow to a much greater extent than the skeletal portion 10. Ideally, the bearing pads 50 and the skeletal portion 10 deflect so as to form a wedge across the entire circumferential face of the bearing pads 50. When a wedge is created across the entire face of the bearing pad, optimum results are achieved because the greatest possible hydrodynamic advantage is generated.
i i---L i For any particular application, the bearing of the present invention must be designed so as to deflect in a manner which allows formation of a hydrodynamic wedge across the entire innermost circumferential face of the bearing pads. Various factors must be taken into account to design a bearing to deflect in such a manner.
For instance, the degree of shear and radial load applied, the flexibility of the materials employed in the bearing pad and skeletal portion, the size and shape if the inner and outer axial grooves and the flexibility of the bearing pads and skeletal portion all must be considered.
The flexibility of the bearing pad and skeletal portion is ultimately a consequence of the design of the bearing. For instance, the flexibility of these elements can obviously be varied by varying the type of material employed in the bearing pads and skeletal portions. The flexibility is also influenced by the size, shape and circumferential positioning of the inner and outer axial grooves. In accordance with an important aspect of the present invention, the o flexibility of the bearing pads 'and skeletal portions 0 1 may also bn, influenced by p--oviding non-newtonian fluidic material in all or part af either the outer or inner axial grooves. For example, as shown in FIG. 1, each of the outer axial grooves 14 are substantially completely filled by deflection control members While in the illustrated embodiment, deflection control members 80 are provided only in the outer axial grooves, it is possible to provide deflection control members in g the inner axial grooves as well. In any instance, the control -members are preferably fused to either the skeletal portion and/or the bearing pad.
In the illustrated example, the deflection control members 80 are of a relatively soft or flexible -16non-newtonian fluidic material preferably an elastomer or polymer such as rubber plastic or the like. For example, Shore A soft durometer rubber could be used to form the deflection control members as well as the bearing pads. Alternatively, different materials could.
be used depending upon the degree of deflection control required or desired. As shown in FIG. 1, the deflection control members 80 have the same shape as the outer axial grooves 14. Accordingly, the deflection control members 80 fill the axial grooves 14 completely.
However, this is not necessarily so. Specifically, it is possible that the deflection control members could be provided so as to only partially fill the grooves 14.
This would of course, effect the degree of deflection control provided by the deflection control members.
The deflection control members 80 act by filling the grooves to a predetermined extent so as to limit the flexibility in the shear direction of the SD skeletal portion 10. It follows that the degree of n limiting of the flexibility of the skeletal portion O0 depends upon the degree to which the deflection control t members fill the inner and outer grooves and the flexibility of the material used in the deflection control members. It is also possible that the deflection control members could be constructed of the same material as the bearing pads and be formed to be unitary therewith. It is noted that with a filled grove the radial restraint is high while in the shear or circumferential direction the flexibility is high. In other words, the overall pad structure is stiff in the radial direction and flexible in the shear direction to form a wedge for hydrodynamic lubrication.
As previously noted, the bearing of the present invention is preferably constructed entirely of non-newtonian fluidic materials preferably polymeric or 1 1 I il-- i il- YI
I-I
-17elastomeric such as rubber, plastic and the like. By virtue of its construction entirely of such fluid materials, the bearing of the present invention exhibits a number of unique performance characteristics. For instance, the high radial stiffness combined with the inward movement of the pad results in accurate shaft positioning and optimun fluid film formation. Film formation reduces shaft wear and provides for high load carrying capability. Additionally, bearings constructed of non-newtonian fluidic materials such as elastomers exhibit exceptional abrasion resistance in process lubricated applications. Finally, some non-newtonian fluidic materials such as elastomers and polymers are also resistant to coirosion by substances which corrode non-fluidic materials such as metals. The need for radial stiffness and the need for abrasion resistance have heretofore been believed incompatible. However, the use of a multi-durometer composite consisting entirely of non-newtonian fluidic materials makes it C possible to achieve both beneficial results. Finally, some non-newtonian fluidic materials such as elastomers and polymers are also resistant to corrosion by 0 0 substances which corrode non-fluidic materials such as 0 0 metals.
The non-newtonian fluidic materials used in the bearings of the present invention are restrained E along their outer pheriphery by the housing in which the bearing is located. Accordingly, the bearings are constrained to deflect or bulge along the axial end portions which are not restrained. The degree of bulging of the bearings out of the unrestrained axial ends thereof is indicative of the radial stiffness of the bearing. The degree of bulging, and hence the bearings radial stiffness, depends on the size or area of unrestrained non-newtonian fluidic material and the stiffness of the non-newtonian fluidic material used.
VIP
-18- 00 0 a 03 o o 0 0 0 00 0 0 0 0o O 0 0 o 0 0 0 *0 00 0 S0 0 0 00 80 *0 000 00 0 0 As noted above, conventional cutless or weartype journal bearings are typically constructed of a single durometer elastomer mounted in a metal cylinder.
Because the metal is incompressible, relatively large sections of soft durometer material must be provided.
Accordingly, and because there is nothing to restrain the relatively large sections of material, these bearings exhibit a relatively large amount of bulge out of the axial ends of the bearings. The great degree of bulge means that the bearing has very little radial stiffness. Of course, this is expected given the large cross section of unrestrained area and the soft material used. In response to the load of a shaft, these bearings typically deform so as to conform to the shape of the shaft such that a true hydrodynamic wedge is not formed. Thus, these wear-type bearings function mainly as elastomeric wear sleeves for the shaft. The resulting contact between the bearing pads and the shaft can generate E great deal of heat which can alter the material chara.:teristics of the bearing pad material and thereby reduce the life expectancy of the bearing.
Since, as shown in Figure 1, the relatively stiff skeletal portion 10 is a large portion of the axial cross section of the bearings of the present invention, the unrestrained cross-sectional area of the relatively soft durometer material in the bearings of the present invention is significantly reduced. In particular, because the skeletal portion 10 is constructed of a relatively stiff material, it is not subject to a great deal of such bulging. Accordingly, only the materials used in the sections 80 and bearing pads 50 are subject to appreciable axial.bulging. In other words, the cross section bulge area of the bearings of the present invention is significantly reduced from that of prior art wear-type bearings.
Thus, the provision of the relatively stiff skeletal eY- -19portion provides the bearing with much greater radial stiffness. As a result of this radial stiffness, the bearing of the present invention forms a hydrodynamic wedge which allows the bearings of the present invention to carry a far greater load and, more importantly, reduces the wear on the bearings thereby increasing the life expectancy of the bearings. Thus, another significant advantage of the present invention is the reduction of bulging of the axial ends of the bearing which increases the radial stiffness of the bearing and reduces wear.
QO 0 0 0 4 o 00 0 0 ci 0 00 0 00 o a a00C O 0 c Ci, 0 o 00 i ci i i Oci 40440t In summary the bearing of the present invention includes a generally circumferential skeletal portion formed of a relatively rigid non-newtonian fluid. A plurality of inner axially extending radial grooves are formed on the inner circumference of the skeletal portion. The inner axial grooves are circumferentially spaced with respect to one another.
The skeletal portion also can include a plurality of outer axial grooves preferably equal in number to the inner axial grooves and spaced about the outer circumference of the skeletal portion preferably centered about a mid point which is directly between two opposed inner axial grooves. The bearing further includes a plurality of bearing pads equal to a number to the inner axial grooves and fused to portions of the skeletal portion defined by the inner axial grooves and fused thereto. The bearing may also include deflection control members located in the inner axial grooves and/or the outer axial grooves. The deflection control members may fill entirely the axial grooves or only partially fill the axial grooves.
With the bearing construction described above, it is possible to achieve virtually any desired deflection in response to a known or determinable load.
K I specifically, the bearing pad support is capable of movement with six degrees of freedom. In contrast, the bearing pad support of conventional wear-type bearings cannot move in the radial direction. The tendency of the bearing pads to deflect and the degree of deflection under a known load may be varied by varying a number of different parameters. First, the degree of deflection can be varied by varying the cross-section of the bearing. specifically, the number and depth of the inner and outer axial grooves and the circumferential dimensions of the bearing pads and skeletal portion define the beam network for supporting the bearing pads and consequently influence the degree of deflection of the bearing pads under load.
Further, the choice of materials for the various components of the bearing affects the deflection 0 characteristics of the bearing. In this regard, the 0 00 hardness or flexibility of the non-newtonian fluidic :o 0 material employed is the most critical characteristic to 0 be taken into .onsideration.
Finally, the size and location of the deflection control members influences the deflection 00$4 characteristics of the bearing. Ini extreme cases, the deflection control member can be constructed of the same material as the skeletal portion so, for practical purposes, that the skeletal portion does not include the.
outer axial crrooves. In the other extreme case, the F outer axial grooves or the inner axial grooves can be left completely unfilled to allow free, unrestrained *deflection. In summary, by varying the foregoing parameters, bearings can be designed in accordance with the present invention to achieve virtually any desired deflection.
In designing bearings in accordance with the -21present invention, several points should be kept in mind. Foremost among these is the need to maintain an extrudable cross-section such as a constant crosssection in the bearing, when the axial cross section of the bearing is constant, the bearing can be easily extruded as discussed below at a tremendously low cost.
Naturally, the deflection charact-tristics of the bearing can be varied by varying the cross-section of the individual bearing such as by providing circumferential grooves, partial radial grooves or radial ')ores.
However, such variations from the preferred constant cross-section require additional machining after the extrusion and sizing (machining of the inner and outer diameters) of the bearing and should therefore be avoided unless the resulting performance benefits 00 justify the increased cost of manufacture.
0 0 0 00 The bearings of the present invention also may 00 0 be generally characterized as multi-durometer bearings 0 since they iri ,lude multiple sections having different durometers (degrees of rigidity) Specifically, higher 00 durometer (more rigid) non-newtonian fluids are used for strength and low durometer (more flexible) non-newtonian 0: fluidic materials are used for flexibility. The various 0 durometer sections are fused together. For instance, in 0 the bearing illustrated different materials could be used for the skeletal portion, the bearing pads and the deflection control members. Generally, more rigid materials would be used for the skeletal portion and less rigid, more flexible, materials would be used for the bearing pads and deflection control members.
The novel bearing of the present invention may be made in accordance with a novel method of manufacture which is discu-.sed hereinafter with reference to FIG. As indicated in FIG. 5, the method of making a _LUUL±udF-ea applications such as oil well drilling applicatio~ns, submersible or turbine pump applications and marine drive shaft applications.
-22bearing in accordance with the present invention involves four general steps, to wit, extrusion, curing, cutting and sizing.
The first step, extrusion, involves two or more sub-steps of the number of sub-steps depends upon the number of different materials to be used in the bearing and the location of the various bearing sections. It should be pointed out that the bearing is extruded using known multi-durometer extrusion techniques which are commonly employed in extruding plastic components such as window and door seals, shock absorbing bumpers, and flexible hinges. In the example illustrated in FIG. 5, three extrusion sub-steps are employed. This corresponds to the number of extrusion sub-steps which would be preferably be used to form a 0 0 bearing of the type shown in FIG. 1.
0 OR the At the first sub-step 101, a first portion of 0the bearing is extruded. In the example illustrated in 00 0 producing the bearing illustrated in FIG. 1, the f irst 00 0 0 0 portion to be extruded would presumably be the inner portion 50. This portion would be extruded in an uncured 0 0 or partially cuired state.
Step 102 closely follows step 101 and involves the extrusion of a second portion onto the uncured or 4 4 6 partially cured first portion. In extruding the bearing illustrated in FIG. 1, strp 102, would presumably involve the extrusion of the skeletal portion 10 onto the associated portion of the pad face After completion of step 102, if additional bearing sections are required, they are extruded in further extrusion sub-steps In extruding the bearing illustrated in FIG. 1, a third extrusion sub-step 103 is performed. During this extrusion sub-step the outer 1K w
L"
-23deflection control members 80 are extruded into the outer axial grooves.
It is important to note that each successive extrusion is uncured or only partially cured so that it is not necessary to apply an adhesive to j:in the successive extrusions during the extrusion process.
Specifically, in the uncured or partially cured state in non-newtonian fluidic materials employed in the bearings of the present invention are gummy or tacky such that no adhesive is necessary to adhere the successive excretion extrusions. This, in accordance with the present invention, the bearing sections are fused to one another without the aid of a foreign substance such as an adhesive.
II
V Y Completion of the extrusion process yields a composite uncured or partially cured tubular extrusion.
After the extrusion process is completed, the composite tubular extrusion is cured at step 104 to yield a cured tubular extrusion in which the various bearing sections C having varied durometers are fused to one another.
FIG. 2 illustrates an example of a tubular extrusion in accordance with the present invention. As suggested by FIG. 2, the extrusion is preferably quite long so that a large number of bearings can be formed from any one extrusion.
At step 105, the curea tubular extrusion is cut into segments having axial thicknesses corresponding to the desired axial thickness of the bearing. In other words, a tubular extrusion is divided into bearing segments. For example, one tubular extrusion, such as that shown in FIG. 2, may be divided into 40-50 individual bearing segments.
-24- In step 106, the individual bearing segments are sized. In the simplest and preferred embodiment, the sizing step simply involves machining the bearing segments to define precisely the desired inner and outer diameters. Naturally, this step is only possible if the tubular extrusion has a outer diameter which is larger than the desired outer diameter and an inner diameter which is smaller than the desired inner diameter. In FIG. 1, the phantom lines illustrate generally, the degree of extra material which should be provided to insure that the bearing segments can be properly sized.
The sizing step 106 can also involve additional machining of the bearing segments to the extent cost of such machining is justified by the improved performance derived by the additional machining. For instance, it may also be desirable to So° provide non-uniformities in the cross-section of the 00 C bearing segments such as circur.ferential grooves and o 6O o radial bores. Such steps, which can potentially add a great deal to the cost of individual bearings, would normally not be justified, particularly since a wide variety of deflection characteri3tics can be achieved, 00 0 o000 as discussed above, while maintaining a constant OJ extrudable bearing cross-section.
0 00 0 o 00a.
0 S00 «i -e

Claims (7)

1. A hydrodynamic bearing for su characterized in that the bearing imaterials and includes a generally I support portion having a predeter i having inner and outer circumfereni illows: pporting a shaft on a fluid film is formed of non-newtonian fluidic circumferential skeletal bearing pad mined hardness, the skeletal portion tial surfaces; tt a plurality of inner axial grooves formed in the inner surface and spaced circumferentially so as to define a plurality of beam mounted bearing pad support surfaces; a plurality of bearing pads having a predetermined hardness which is less than the predetermined hardness of the skeletal portion, each one of the plurality of bearing pads being fused to a corresponding pad support surface.
2. The bearing of claim 1, wherein the axial cross-section of the bearing is constant so that the bearing can be easily extruded.
3. The bearing of claim 1 or claim 2 wherein said adjacent sections of dissimilar materials are fused together.
4. The bearing of any one of claims 1-3 wherein a plurality of radially inwardly extending outer grooves are formed in the outer circumferential surfaces, the outer grooves being spaced circumferentially about the outer circumferential surface. 2561050/256 10/01/91
26. The bearing of claim 4 wherein the outer grooves and inner groves are spaced with respect to one another so as to define a skeletal bearing pad support portion having beam mounted bearing pad support surfaces which can move with six degrees of freedom. 6. The bearing of any one of claims 1-5 further comprising a plurality of deflection control members formed in at least one of said radially outwardly extending inner groves and radially inwardly extending outer o a grooves. 0 0 0 0 0 o no 0o0o 7. The bearing of any one of claims 1-6 wherein each said bearing pad is 0 o0 00 00 S° generally concave in axial cross-section and has circumferential ends in ^o o its unstressed state, the bearing pad having an axis of symmetry 0 0 equidistant from said circumferential ends and said bearing pad having a greater radial thickness along said axis of symmetry than at either of o 3 0 said circumferential ends. 8. The bearing of any one of claims 1-7 wherein said skeletal portion is a unitary element. 9. The bear-lig of any one of claims 1-5, 7 or 8 in which a plurality of deflection control members are positioned in at least one of said inner and outer grooves, said deflection control members having a predetermined hardness which is less than the hardness of the skeletal portion. The bearing of claim 9 wherein at least one of said deflection control members is formed of the same material as at least one of said bearing pads and is unitary therewith. .i2561050/256 10/01/91 L .r _L C I- Y1LU the greatest generated. possible hydrodynamic advantage is
27. 11. The bearing of claim 9 wherein said deflection control members are formed of a material having a hardness different than the predetermined hardness of the bearing pad. 12. The bearing of any one of claims 6 or 9 to 11 wherein the deflection control members are fused to the skeletal bearing pad support portion. 13. A method for making a hydrodynamic bearing of any one of claims 1 to 12, said method comprising the steps of extruding a first tubular element of a naterial having a predetermined cured hardness; extruding onto said first portion a second portion from a material having a second predetermined cured hardness, which is different than the first predetermined cured hardness, to form a composite tubular extrusion; curing the composite tubular extrusion; cutting the tubular extrusion into bearing segments; and sizing the bearing segments. 0 1 0 04 o .34 o .3c '0 03.3 .3 0 .3 0 '0i 00 0 0 0 00 000 0) 09R 0 0O 0 0 .3 0 .3 0. 0 .a a .3o .3 .333... .3 .3 14. The method of claim 13 further comprising the step of extruding a third portion onto at least one of said first portion and said second portion prior to curing the composite tubular extrusion. The method of claim 13 or claim 14 wherein the step of sizing the bearing segments includes the step of machining the bearing segments so as to provide non-uniformities in the axial cross-section of the bearing segments. 16. A hydrodynamic bearing for supporting a shaft on a fluid film, said bearing being substantially as hereinbefore described with reference to any one of Figs. 1 to 4. 2561050/256 10/01/91 t '2561050/256 10/01/91 r_ L i i .)iC C I- U-U i L-i .il i ~I(
28. 17. A hydrodynamic bearing for supporting a shaft on fluid film, said bearing being substantially as hereinbefore described with reference to any one of Figs 1 to 4. Dated this day of Janaury 1991. 00 o o o0 C00' o0 00' 0 0 00 l o 0 00 00 RUSSELL D. IDE By his solicitors Freehilli Hollingdaie Page 0' 000000 0000' C 0 00 0 0 00~000 0 0 0 00 0 0 0 00 00 0 0 0 00 I A 2561050/256 10/01/91 ABSTRACT OF THE DISCLOSURE An extrudable multi-durometer hydrodynamic bearing which includes a bearing pad support structure and a plurality of bearing pads fused to the bearing pad support structure. The bearing may also include a number of deflection control members fused to the bearing pads and/or the bearing pad support structure. The pad supports of the bearing and movable with six degrees of freedom. The bearing is constructed entirely of non- newtonian fluidic materials and has a constant axial 0I 004 cross-section so that it may be easily extruded. The 0o 0 0bearing includes portions having different hardnesses. 0 The method of making the bearing includes the steps of extruding a first material, extruding at least a second material onto the first material prior to curing the first material forming a tubular extrusion, nd acuring the tubular extrusion, cutting the tubular extrusion into bearing segments and sizing the bearing segments by machining the individual bearing segments to the desired inner and outer diameters. 1 f d e b C, netna lidcmtras n a ontn xa hL L I tl. I -L.ULII- ~L
AU33892/89A 1988-10-25 1989-05-01 Extrudable multi-durometer hydrodynamic bearing and method of making the same Ceased AU613185B2 (en)

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